Functional control subsystems missiles "air-to-air" short-range


Аuthors

Obnosov B. V.1, Daneko A. I.1, Zakharov I. V.2*, Trubnikov A. A.3**, Reshetnikov D. A.3***

1. ,
2. ,
3. Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: il-ya-zakharov@yandex.ru
**e-mail: a-trubnikov@inbox.ru
***e-mail: grapler@yandex.ru

Abstract

The article deals with image and methodological support of hardware and software for the rapid assessment of the technical condition of missile class "air-to-air" short range of the operating organization with the application of the method of functional control.

Keywords:

functional control, hardware and software, missile control system, linear acceleration sensors, angu-lar acceleration sensors


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